An approximate method of calculating three-dimensional, compressible flow in axial turbo-machines.
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An approximate method of calculating three-dimensional, compressible flow in axial turbo-machines.
- Publication date
- 1953
- Topics
- Aeronautics
- Publisher
- California Institute of Technology
- Collection
- navalpostgraduateschoollibrary; fedlink; americana
- Contributor
- Naval Postgraduate School, Dudley Knox Library
- Language
- en_US
Thesis (MS)--Iowa State College, 1953
Bibliography: p. 38
Bibliography: p. 38
- Addeddate
- 2011-09-20 04:05:16
- Call number
- ocn640229637
- Camera
- Canon EOS 5D Mark II
- Degree.grantor
- California Institute of Technology
- Degree.level
- doctoral
- Degree.name
- Ph.D.
- Description.service
- U.S. Navy (U.S.N.) author.
- External-identifier
-
urn:handle:10945/13953
urn:oclc:record:1039950593
- Foldoutcount
- 0
- Identifier
- approximatemetho00holm
- Identifier-ark
- ark:/13960/t0tq6w771
- Identifier.oclc
- ocn640303321
- Ocr_converted
- abbyy-to-hocr 1.1.37
- Ocr_module_version
- 0.0.21
- Openlibrary_edition
- OL24991697M
- Openlibrary_work
- OL16095883W
- Page-progression
- lr
- Page_number_confidence
- 0
- Page_number_module_version
- 1.0.3
- Pages
- 226
- Ppi
- 350
- Scandate
- 20110921025847
- Scanner
- scribe7.sanfrancisco.archive.org
- Scanningcenter
- sanfrancisco
- Type
- Thesis
- Full catalog record
- MARCXML
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